View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65915U 26145.47219740 +.00000000 +00000-0 +93433-3 0 00006
2 65915 53.1585 169.0673 0000995 81.7853 278.3261 15.30198765 06
| Epoch (UTC): | 25 May 2026 11:19:57 |
| Eccentricity: | 0.0000995 |
| inclination: | 53.1585° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.0673° |
| argument of perigee: | 81.7853° |
| revolutions per day: | 15.30198765 |
| mean anomaly at epoch: | 278.3261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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